- Location
-
Deutsche Nationalbibliothek Frankfurt am Main
- ISSN
-
2524-6992
- Extent
-
Online-Ressource
- Language
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Englisch
- Notes
-
online resource.
- Bibliographic citation
-
Notes on the hypersonic boundary layer transition ; volume:4 ; number:1 ; day:20 ; month:5 ; year:2022 ; pages:1-2 ; date:12.2022
Advances in aerodynamics ; 4, Heft 1 (20.5.2022), 1-2, 12.2022
- Creator
-
Zhu, Wenkai
- Contributor
-
SpringerLink (Online service)
- DOI
-
10.1186/s42774-022-00117-x
- URN
-
urn:nbn:de:101:1-2022072222502349119523
- Rights
-
Open Access; Der Zugriff auf das Objekt ist unbeschränkt möglich.
- Last update
-
15.08.2025, 7:29 AM CEST
Data provider
This object is provided by:
Deutsche Nationalbibliothek. If you have any questions about the object, please contact the data provider.
Deutsche Nationalbibliothek. If you have any questions about the object, please contact the data provider.
Associated
- Zhu, Wenkai
- SpringerLink (Online service)
Other Objects (12)
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Effects of discrete roughness elements on laminar-turbulent transition in a hypersonic boundary layer
Passive hypersonic boundary layer transition control using ultrasonically absorptive carbon-carbon ceramic with random microstructure
Roughness-Induced Transition in a Hypersonic Capsule Boundary Layer under Wind-Tunnel and Reentry Conditions
Direct numerical simulation of hypersonic boundary layer transition over a lifting-body model HyTRV
Numerical simulation of turbulent shock boundary layer interactions in hypersonic flows
Experiments on a smooth wall hypersonic boundary layer at Mach 6
Experimental study of bluntness effects on hypersonic boundary-layer transition over a slender cone using surface mounted pressure sensors
A symmetry-based length model for characterizing the hypersonic boundary layer transition on a slender cone at moderate incidence
Numerical Investigation of the Hypersonic Laminar-Turbulent Boundary-Layer Transition around a Blunted Cone in CO2, Mars and Earth Atmospheres
Research Progress of hypersonic boundary layer transition control experiments
Controlling hypersonic boundary layer transition with localized cooling and metasurface treatments
Experimental investigations of hypersonic boundary layer transition on a re-entry capsule
Effects of discrete roughness elements on laminar-turbulent transition in a hypersonic boundary layer
Passive hypersonic boundary layer transition control using ultrasonically absorptive carbon-carbon ceramic with random microstructure
Roughness-Induced Transition in a Hypersonic Capsule Boundary Layer under Wind-Tunnel and Reentry Conditions
Direct numerical simulation of hypersonic boundary layer transition over a lifting-body model HyTRV
Numerical simulation of turbulent shock boundary layer interactions in hypersonic flows
Experiments on a smooth wall hypersonic boundary layer at Mach 6
Experimental study of bluntness effects on hypersonic boundary-layer transition over a slender cone using surface mounted pressure sensors
A symmetry-based length model for characterizing the hypersonic boundary layer transition on a slender cone at moderate incidence
Numerical Investigation of the Hypersonic Laminar-Turbulent Boundary-Layer Transition around a Blunted Cone in CO2, Mars and Earth Atmospheres
Research Progress of hypersonic boundary layer transition control experiments
Controlling hypersonic boundary layer transition with localized cooling and metasurface treatments
Experimental investigations of hypersonic boundary layer transition on a re-entry capsule
Effects of discrete roughness elements on laminar-turbulent transition in a hypersonic boundary layer
Passive hypersonic boundary layer transition control using ultrasonically absorptive carbon-carbon ceramic with random microstructure
Roughness-Induced Transition in a Hypersonic Capsule Boundary Layer under Wind-Tunnel and Reentry Conditions
Direct numerical simulation of hypersonic boundary layer transition over a lifting-body model HyTRV
Numerical simulation of turbulent shock boundary layer interactions in hypersonic flows
Experiments on a smooth wall hypersonic boundary layer at Mach 6
Experimental study of bluntness effects on hypersonic boundary-layer transition over a slender cone using surface mounted pressure sensors
A symmetry-based length model for characterizing the hypersonic boundary layer transition on a slender cone at moderate incidence